EN 
卢少鹏
副研究员
williamhill威廉希尔官网A341
lusp@sjtu.edu.cn
教育背景
- 2003年-2007年，哈尔滨工业大学，学士
- 2007年-2010年，哈尔滨工业大学，硕士
- 2010年-2014年，哈尔滨工业大学，博士
工作经历
- 2020年-至今，williamhill威廉希尔官网，副研究员
- 2014年-2020年，williamhill威廉希尔官网，博士后、专职科研人员
研究方向
- 1、叶轮机械气动热力学：燃气轮机传热及冷却、气动设计及优化、非定常传热机理及应用
- 2、航空电推进系统：推进系统噪声抑制、推进系统综合热管理
- 3、航空动力智能应用：AI驱动航空发动机气热设计、气热实验及数值的深度学习应用
- 4、微型飞行器动力系统：低空飞行器综合热管理、流动控制及噪声抑制
主要科研项目
- 高压涡轮转子叶片叶尖及端壁流动传热特性研究
- XXXXX低压涡轮叶冠多学科精细化设计
- 高压涡轮工作叶片长时服役后气动热力性能研究
- 先进重型燃机高负荷动叶顶部间隙泄漏流抑制技术研究
- XXXXX发动机涡轮动叶叶尖换热特性试验
- 端区泄漏损失机理及控制方法研究
- 涡轮叶片典型冷却结构流阻及换热特性试验研究
- 涡轮叶片典型冷却单元及其组合结构的传热与流阻特性试验研究
- 航空科学基金：小间隙跨音速高压涡轮叶尖传热特性实验研究
- 自然科学基金：气冷涡轮叶尖泄漏流动的高低速模化设计及实验研究
- 自然科学基金：气冷涡轮动叶叶顶多目标拓扑优化研究
- 国家科技重大专项：过渡态涡轮叶尖换热特性数值模拟及试验技术研究
- 上海市科技创新专项：陶瓷基复合材料高压涡轮导叶热分析及冷却设计技术研究
代表性论文专著
- Lu S, Wang Y, Jiang H, et al. Thermal concentration and cooling characteristics of a rotating turbine blade tip with different tip clearances[J]. International Journal of Heat and Mass Transfer, 2026, 254: 127647.
- Li J, Wang Z, Jiang H, Lu S*, et al. Influence of anisotropic thermal conductivity on leading edge cooling performance of a film cooled CMC turbine vane[J]. International Journal of Thermal Sciences, 2026, 220: 110360.
- Lu S, Gu H, Jiang H, et al. Investigation on striped heat transfer characteristics of turbine blade tips[J]. Physics of Fluids, 2025, 37(1).
- Li H, Zhang Z, Lu S*, et al. Investigation of film cooling performance of squealer high-pressure turbine blade tip with inclined shelf and partition rib designs[J]. International Journal of Thermal Sciences, 2025, 218: 110173.
- Zhang Z, Lu S*, Jiang H, et al. Effects of Cutback Tip Trailing Edge Squealer on Turbine Blade Tip Thermal Behaviour Under High-Speed Relative Casing Motion[J]. Journal of Turbomachinery, 2025, 147(10): 101016.
- Peng X, Jiang H, Lu S*. Cooling Injection Effect on the Suction Side Near-Tip Region of Turbine Blade With High-Speed Relative Casing Motion[J]. Journal of Turbomachinery, 2025, 147(4): 041009.
- Peng X, Jiang H, Lu S*, et al. Experimental Study on the High Relative Casing Motion Effect on Turbine Blade Tip Aerodynamic Characteristics[J]. Journal of Turbomachinery, 2025, 147(11).
- Hu S, Li J, Lu S*, et al. Influence of multi-parameter dispersion on thermal conductivity of CMCs and thermal performance of turbine blades[J]. Journal of Physics D: Applied Physics, 2025, 58(35): 355501.
- Peng X, Jiang H, Lu S*. Cooling Injection Effect on the Suction Side Near-Tip Region of Turbine Blade With High-Speed Relative Casing Motion[J]. Journal of Turbomachinery, 2025, 147(4): 041009.
- Peng X, Jiang H, Lu S*, et al. Aerodynamic Feasibility Investigation of the Novel Experimental Rig on Turbine Blade Tip With High Relative Motion[J]. Journal of Engineering for Gas Turbines and Power, 2025, 147(4): 041001.
- Jiang H, Zhang Z, Lu S*, et al. Experimental study on aerodynamic performance of turbine blade squealer tip with different trailing edge designs under high-speed relative casing motion[J]. Aerospace Science and Technology, 2024, 155: 109640.
- Xie W, Lu S*, Jiang H, et al. Interaction mechanism of transonic squealer tip cooling with the effect of high-speed relative casing motion[J]. Journal of Turbomachinery, 2023, 145(8): 081016.
- Lu S, Zhang Q, He L. A high-speed disk rotor rig design for tip aerothermal research[J]. Journal of Turbomachinery, 2022, 144(5): 051002.
- Lu S, Deng Q, Ligrani P M, et al. Effects of coolant and wall temperature variations on impingement jet array thermal performance[J]. Numerical Heat Transfer, Part A: Applications, 2021, 79(1): 68-82.
- Wang W, Lu S*, Jiang H, et al. Influence of tip clearance and cavity depth on heat transfer in a cutback squealer tip[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2021, 235(8): 912-923.
- Lu S, Ma H, Zhang Q, et al. Cutback squealer tip trailing edge cooling performance[J]. International Journal of Heat and Mass Transfer, 2020, 154: 119632.
- Zhu D, Zhang Q, Lu S*, et al. Relative casing motion effect on squealer tip cooling performance at tight tip clearance[J]. Journal of Thermal Science and Engineering Applications, 2020: 1-18.
- Jiang H, Zhang Q, He L, Lu S*, et al. Experimental evidence of temperature ratio effect on turbine blade tip heat transfer[J]. Journal of Turbomachinery, 2018, 140(12): 121010.
- 蒋红梅,张子扬,卢少鹏*.凹槽叶尖尾缘设计对高压涡轮气动性能的影响[J].航空动力学报,2024,39(06):201-211.
- 王维杰, 卢少鹏*, 马海腾, 等. 高压涡轮尾切凹槽叶尖冷却换热特性[J]. 航空动力学报, 2019, 34(10): 2131-2139.
- 《燃气涡轮气动优化设计体系》 2019.09 哈尔滨工业大学出版社
专利著作
- 模拟轴流压气机高速旋转轮毂的悬臂静子平面叶栅实验方法
- 适用于高速旋转机匣的模拟实验器装置
学术兼职
- 《热能动力工程》 编委
- Aerospace Science and Technology、Physics of Fluid、 Journal of Aerospace Engineering 、Journal of Applied Thermal Engineering、International Journal of Heat and Mass Transfer、Journal of Thermal Science、Applied Thermal Engineering等期刊审稿人
荣誉奖励
- 中国航发商用航空发动机有限责任公司技术发明 三等奖